High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
By: Robert S. Jankovsky and Timothy D. Smith, Albert J. Pavli.
Contributors: Smith, Timothy D.; Pavli, Albert J.; NASA Glenn Research Center.
Series: NASA/TP -- 1999-208522; NASA technical paper -- 208522.
Publisher: National Aeronautics and Space Administration, Glenn Research Center; National Technical Information Service, distributor
Published: 1999
Place of publication: [Cleveland, Ohio]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Boundary layer thickness.; Rocket nozzles.; Combustion chambers.; Heat transfer.; Pressure distribution.; Pressure measurement.; Flux (Rate); Heat flux.; Turbulence.
Other titles: High area ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
Notes: Shipping list no.: 2000-0048-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 1 microfiche.